EP3244014A3 - Bague de retenue - Google Patents
Bague de retenue Download PDFInfo
- Publication number
- EP3244014A3 EP3244014A3 EP17158977.3A EP17158977A EP3244014A3 EP 3244014 A3 EP3244014 A3 EP 3244014A3 EP 17158977 A EP17158977 A EP 17158977A EP 3244014 A3 EP3244014 A3 EP 3244014A3
- Authority
- EP
- European Patent Office
- Prior art keywords
- retaining ring
- engine component
- terminal portion
- thickness
- engine
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/30—Fixing blades to rotors; Blade roots ; Blade spacers
- F01D5/3007—Fixing blades to rotors; Blade roots ; Blade spacers of axial insertion type
- F01D5/3015—Fixing blades to rotors; Blade roots ; Blade spacers of axial insertion type with side plates
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
- F01D11/005—Sealing means between non relatively rotating elements
- F01D11/006—Sealing the gap between rotor blades or blades and rotor
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2220/00—Application
- F05D2220/30—Application in turbines
- F05D2220/32—Application in turbines in gas turbines
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2240/00—Components
- F05D2240/20—Rotors
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2260/00—Function
- F05D2260/30—Retaining components in desired mutual position
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2260/00—Function
- F05D2260/94—Functionality given by mechanical stress related aspects such as low cycle fatigue [LCF] of high cycle fatigue [HCF]
- F05D2260/941—Functionality given by mechanical stress related aspects such as low cycle fatigue [LCF] of high cycle fatigue [HCF] particularly aimed at mechanical or thermal stress reduction
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
- F16B21/00—Means for preventing relative axial movement of a pin, spigot, shaft or the like and a member surrounding it; Stud-and-socket releasable fastenings
- F16B21/10—Means for preventing relative axial movement of a pin, spigot, shaft or the like and a member surrounding it; Stud-and-socket releasable fastenings by separate parts
- F16B21/16—Means for preventing relative axial movement of a pin, spigot, shaft or the like and a member surrounding it; Stud-and-socket releasable fastenings by separate parts with grooves or notches in the pin or shaft
- F16B21/18—Means for preventing relative axial movement of a pin, spigot, shaft or the like and a member surrounding it; Stud-and-socket releasable fastenings by separate parts with grooves or notches in the pin or shaft with circlips or like resilient retaining devices, i.e. resilient in the plane of the ring or the like; Details
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US15/154,351 US10215037B2 (en) | 2016-05-13 | 2016-05-13 | Contoured retaining ring |
Publications (4)
Publication Number | Publication Date |
---|---|
EP3244014A2 EP3244014A2 (fr) | 2017-11-15 |
EP3244014A3 true EP3244014A3 (fr) | 2017-12-27 |
EP3244014B1 EP3244014B1 (fr) | 2021-01-20 |
EP3244014B8 EP3244014B8 (fr) | 2021-03-31 |
Family
ID=58213033
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP17158977.3A Active EP3244014B8 (fr) | 2016-05-13 | 2017-03-02 | Ensemble de bague de retenue pour moteur à turbine à gaz |
Country Status (2)
Country | Link |
---|---|
US (1) | US10215037B2 (fr) |
EP (1) | EP3244014B8 (fr) |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2584097A (en) * | 2019-05-20 | 2020-11-25 | Cross Mfg 1938 Limited | Ring fastener |
US11168615B1 (en) | 2020-08-25 | 2021-11-09 | Raytheon Technologies Corporation | Double ring axial sealing design |
US11686202B1 (en) * | 2021-12-20 | 2023-06-27 | Rolls-Royce North American Technologies Inc. | Rotor damper with contact biasing feature for turbine engines |
Citations (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2198780A (en) * | 1986-12-19 | 1988-06-22 | Gen Electric | Retainer ring |
US5281098A (en) * | 1992-10-28 | 1994-01-25 | General Electric Company | Single ring blade retaining assembly |
GB2270544A (en) * | 1992-09-09 | 1994-03-16 | Snecma | Annular seal for a bladed rotor. |
US5338154A (en) * | 1993-03-17 | 1994-08-16 | General Electric Company | Turbine disk interstage seal axial retaining ring |
US20020018719A1 (en) * | 2000-08-10 | 2002-02-14 | Jean-Baptiste Arilla | Rotor blade retaining apparatus |
US20120051918A1 (en) * | 2010-08-27 | 2012-03-01 | Glasspoole David F | Retaining ring arrangement for a rotary assembly |
US20140255196A1 (en) * | 2013-03-08 | 2014-09-11 | United Technologies Corporation | Double split blade lock ring |
WO2014137406A1 (fr) * | 2013-03-08 | 2014-09-12 | Rolls-Royce North American Technologies, Inc. | Agencement de disque, système de rétention, et procédé de retenue de deux éléments rotatifs séparés d'une machine à turbine à gaz |
WO2015088623A2 (fr) * | 2013-09-26 | 2015-06-18 | United Technologies Corporation | Composant rotatif équilibré pour un moteur à gaz |
EP2918785A1 (fr) * | 2014-03-12 | 2015-09-16 | Rolls-Royce plc | Rotor de soufflante |
Family Cites Families (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1638209A (en) * | 1925-10-01 | 1927-08-09 | Niebuhr William Charles | Separable ring |
US4343581A (en) * | 1979-05-21 | 1982-08-10 | Waldes Kohinoor, Inc. | Double-bevel spring retaining ring |
US4752178A (en) * | 1986-12-17 | 1988-06-21 | Smalley Steel Ring Company | Waved retaining ring |
FR2857691B1 (fr) * | 2003-07-17 | 2006-02-03 | Snecma Moteurs | Retention de flasque de rotor |
DE102005048198B4 (de) * | 2005-10-07 | 2007-06-06 | Albrecht Knecht | Sprengring |
FR2913718B1 (fr) * | 2007-03-15 | 2009-06-05 | Snecma Propulsion Solide Sa | Ensemble d'anneau de turbine pour turbine a gaz |
FR2935428B1 (fr) * | 2008-08-26 | 2015-06-26 | Snecma | Aubage fixe de turbomachine a masse reduite et turbomachine comportant au moins un tel aubage fixe |
DE102011082493A1 (de) * | 2011-09-12 | 2013-03-14 | Rolls-Royce Deutschland Ltd & Co Kg | Sicherungssegment zur Schwingungsdämpfung von Turbinenlauf-schaufeln und Rotorvorrichtung |
US20130323052A1 (en) * | 2012-05-31 | 2013-12-05 | Solar Turbines Inc. | Retaining ring |
DE102013223133B3 (de) * | 2013-11-13 | 2014-10-30 | Intellectual Property Management MTU Aero Engines AG | Gasturbine |
US10415401B2 (en) * | 2016-09-08 | 2019-09-17 | United Technologies Corporation | Airfoil retention assembly for a gas turbine engine |
US10392966B2 (en) * | 2016-09-23 | 2019-08-27 | United Technologies Corporation | Retaining ring end gap features |
US10378588B2 (en) * | 2017-01-19 | 2019-08-13 | Gkn Automotive Limited | Retainer for rotating members |
-
2016
- 2016-05-13 US US15/154,351 patent/US10215037B2/en active Active
-
2017
- 2017-03-02 EP EP17158977.3A patent/EP3244014B8/fr active Active
Patent Citations (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2198780A (en) * | 1986-12-19 | 1988-06-22 | Gen Electric | Retainer ring |
GB2270544A (en) * | 1992-09-09 | 1994-03-16 | Snecma | Annular seal for a bladed rotor. |
US5281098A (en) * | 1992-10-28 | 1994-01-25 | General Electric Company | Single ring blade retaining assembly |
US5338154A (en) * | 1993-03-17 | 1994-08-16 | General Electric Company | Turbine disk interstage seal axial retaining ring |
US20020018719A1 (en) * | 2000-08-10 | 2002-02-14 | Jean-Baptiste Arilla | Rotor blade retaining apparatus |
US20120051918A1 (en) * | 2010-08-27 | 2012-03-01 | Glasspoole David F | Retaining ring arrangement for a rotary assembly |
US20140255196A1 (en) * | 2013-03-08 | 2014-09-11 | United Technologies Corporation | Double split blade lock ring |
WO2014137406A1 (fr) * | 2013-03-08 | 2014-09-12 | Rolls-Royce North American Technologies, Inc. | Agencement de disque, système de rétention, et procédé de retenue de deux éléments rotatifs séparés d'une machine à turbine à gaz |
WO2015088623A2 (fr) * | 2013-09-26 | 2015-06-18 | United Technologies Corporation | Composant rotatif équilibré pour un moteur à gaz |
EP2918785A1 (fr) * | 2014-03-12 | 2015-09-16 | Rolls-Royce plc | Rotor de soufflante |
Also Published As
Publication number | Publication date |
---|---|
EP3244014B1 (fr) | 2021-01-20 |
US10215037B2 (en) | 2019-02-26 |
US20170328224A1 (en) | 2017-11-16 |
EP3244014B8 (fr) | 2021-03-31 |
EP3244014A2 (fr) | 2017-11-15 |
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